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 26104.20243328 +.00000000 +00000-0 +35168-4 0 00000
2 21875 82.9231 268.9269 0038312 147.8594 25.2421 13.73959725 04
| Epoch (UTC): | 14 April 2026 04:51:30 |
| Eccentricity: | 0.0038312 |
| inclination: | 82.9231° |
| perigee height: | 957 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 268.9269° |
| argument of perigee: | 147.8594° |
| revolutions per day: | 13.73959725 |
| mean anomaly at epoch: | 25.2421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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