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 26106.89266044 +.00000000 +00000-0 +16692-4 0 00008
2 21875 82.9233 266.9319 0038457 140.5381 11.6257 13.73959881 03
| Epoch (UTC): | 16 April 2026 21:25:25 |
| Eccentricity: | 0.0038457 |
| inclination: | 82.9233° |
| perigee height: | 957 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 266.9319° |
| argument of perigee: | 140.5381° |
| revolutions per day: | 13.73959881 |
| mean anomaly at epoch: | 11.6257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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