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 22638U 26100.16115280 +.00000000 +00000-0 +58761-4 0 00008
2 22638 69.9189 91.9069 0062125 252.2978 107.1359 14.33649794 06
| Epoch (UTC): | 10 April 2026 03:52:03 |
| Eccentricity: | 0.0062125 |
| inclination: | 69.9189° |
| perigee height: | 735 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 91.9069° |
| argument of perigee: | 252.2978° |
| revolutions per day: | 14.33649794 |
| mean anomaly at epoch: | 107.1359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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