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 21875U 26053.71155889 +.00000000 +00000-0 +30600-4 0 00009
2 21875 82.9278 306.3648 0036348 291.0375 122.3037 13.73955116 01
| Epoch (UTC): | 22 February 2026 17:04:38 |
| Eccentricity: | 0.0036348 |
| inclination: | 82.9278° |
| perigee height: | 959 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 306.3648° |
| argument of perigee: | 291.0375° |
| revolutions per day: | 13.73955116 |
| mean anomaly at epoch: | 122.3037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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