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 26100.20590735 +.00000000 +00000-0 +71915-4 0 00005
2 28050 99.0612 77.8562 0051635 103.8774 267.2063 14.17581160 09
| Epoch (UTC): | 10 April 2026 04:56:30 |
| Eccentricity: | 0.0051635 |
| inclination: | 99.0612° |
| perigee height: | 796 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 77.8562° |
| argument of perigee: | 103.8774° |
| revolutions per day: | 14.17581160 |
| mean anomaly at epoch: | 267.2063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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