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 26070.24025962 +.00000000 +00000-0 +56356-4 0 00002
2 21903 82.9411 341.1220 0042008 201.9769 269.7855 13.74743991 03
| Epoch (UTC): | 11 March 2026 05:45:58 |
| Eccentricity: | 0.0042008 |
| inclination: | 82.9411° |
| perigee height: | 952 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 341.1220° |
| argument of perigee: | 201.9769° |
| revolutions per day: | 13.74743991 |
| mean anomaly at epoch: | 269.7855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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