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Satellite Number

CLASSIFICATION_UNCLASSIFIED

Last two digits of launch year

Launch number of the year

Piece of the launch

Epoch
07 Apr 26 00:53 UTC

First Derivative of Mean Motion; the ballistic coefficient (rev/day, per day)

Second Derivative of Mean Motion (rev/day³)

BSTAR, the drag term, or radiation pressure coefficient (units of 1/(Earth radii)

Ephemeris type (always zero; only used in undistributed TLE data)

Element Set Number. Incremented when a new TLE is generated for this object.

1 25544U 98067A 26097.03736053 0.00008175 0 0.00015735 0 999

2 25544 51.6332 292.2025 0.0006344 281.0633 78.9642 15.48812043 56072

Satellite Number

Inclination

Right Ascension of Ascending Node

Eccentricity

Argument of Perigee (degrees)

Mean Anomaly (degrees)

Mean Motion (revolutions per day)

Revolution Number

1 25544U 98067A 26097.03736053 0.00008175 0 0.00015735 0 999

2 25544 51.6332 292.2025 0.0006344 281.0633 78.9642 15.48812043 56072

Satellite Number	25544
Classification	U
Last two digits of launch year	98
Launch number of the year	067
Piece of the launch	A
Epoch 07 Apr 26 00:53 UTC	26097.03736053
First Derivative of Mean Motion; the ballistic coefficient (rev/day, per day)	0.00008175
Second Derivative of Mean Motion (rev/day³)	0
BSTAR, the drag term, or radiation pressure coefficient (units of 1/(Earth radii)	0.00015735
Ephemeris type (always zero; only used in undistributed TLE data)	0
Element Set Number. Incremented when a new TLE is generated for this object.	999

Satellite Number	25544
Inclination	51.6332
Right Ascension of Ascending Node	292.2025
Eccentricity	0.0006344
Argument of Perigee (degrees)	281.0633
Mean Anomaly (degrees)	78.9642
Mean Motion (revolutions per day)	15.48812043
Revolution Number	56072

Ground Position