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 26068.40829653 +.00000000 +00000-0 +63218-4 0 00005
2 21088 82.9466 170.2551 0023099 39.0836 31.3188 13.77494152 06
| Epoch (UTC): | 09 March 2026 09:47:56 |
| Eccentricity: | 0.0023099 |
| inclination: | 82.9466° |
| perigee height: | 956 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 170.2551° |
| argument of perigee: | 39.0836° |
| revolutions per day: | 13.77494152 |
| mean anomaly at epoch: | 31.3188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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