View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 00115U 60002D 25078.29730207 .00009590 00000-0 89996-3 0 9994
2 00115 48.1623 172.3061 0027541 10.2211 349.9260 14.94154975450011
Epoch (UTC): | 19 March 2025 07:08:06 |
Eccentricity: | 0.0027541 |
inclination: | 48.1623° |
perigee height: | 566 km |
apogee height: | 604 km |
right ascension of ascending node: | 172.3061° |
argument of perigee: | 10.2211° |
revolutions per day: | 14.94154975 |
mean anomaly at epoch: | 349.9260° |
orbit number at epoch: | 45001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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