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 28050U 26088.20713029 +.00000000 +00000-0 +81570-4 0 00001
2 28050 99.0597 65.6221 0051317 137.3826 234.5832 14.17577102 07
| Epoch (UTC): | 29 March 2026 04:58:16 |
| Eccentricity: | 0.0051317 |
| inclination: | 99.0597° |
| perigee height: | 797 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 65.6221° |
| argument of perigee: | 137.3826° |
| revolutions per day: | 14.17577102 |
| mean anomaly at epoch: | 234.5832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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