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 26142.57979352 +.00000000 +00000-0 +12616-4 0 00004
2 28054 98.9903 166.2372 0006397 211.6957 320.5628 14.14479820 08
| Epoch (UTC): | 22 May 2026 13:54:54 |
| Eccentricity: | 0.0006397 |
| inclination: | 98.9903° |
| perigee height: | 839 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 166.2372° |
| argument of perigee: | 211.6957° |
| revolutions per day: | 14.14479820 |
| mean anomaly at epoch: | 320.5628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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