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 21088U 26074.28855045 +.00000000 +00000-0 +51376-4 0 00004
2 21088 82.9463 165.8838 0022747 23.1109 30.8833 13.77495047 02
| Epoch (UTC): | 15 March 2026 06:55:30 |
| Eccentricity: | 0.0022747 |
| inclination: | 82.9463° |
| perigee height: | 956 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 165.8838° |
| argument of perigee: | 23.1109° |
| revolutions per day: | 13.77495047 |
| mean anomaly at epoch: | 30.8833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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