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 is defined by the following mean orbital elements,
1 28054U 26032.50270355 +.00000000 +00000-0 +10144-3 0 00005
2 28054 99.0018 55.3534 0007513 164.3877 317.7309 14.14447188 07
| Epoch (UTC): | 01 February 2026 12:03:53 |
| Eccentricity: | 0.0007513 |
| inclination: | 99.0018° |
| perigee height: | 839 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 55.3534° |
| argument of perigee: | 164.3877° |
| revolutions per day: | 14.14447188 |
| mean anomaly at epoch: | 317.7309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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