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 26070.74067078 +.00000000 +00000-0 +65719-4 0 00008
2 21088 82.9465 168.5212 0022957 32.7248 77.3402 13.77494568 08
| Epoch (UTC): | 11 March 2026 17:46:33 |
| Eccentricity: | 0.0022957 |
| inclination: | 82.9465° |
| perigee height: | 956 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 168.5212° |
| argument of perigee: | 32.7248° |
| revolutions per day: | 13.77494568 |
| mean anomaly at epoch: | 77.3402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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