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 21903U 26131.81403558 +.00000000 +00000-0 -50973-4 0 00004
2 21903 82.9338 295.4820 0043329 33.3945 80.2489 13.74742294 02
| Epoch (UTC): | 11 May 2026 19:32:12 |
| Eccentricity: | 0.0043329 |
| inclination: | 82.9338° |
| perigee height: | 951 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 295.4820° |
| argument of perigee: | 33.3945° |
| revolutions per day: | 13.74742294 |
| mean anomaly at epoch: | 80.2489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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