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 21808U 26103.95841551 +.00000000 +00000-0 +31835-3 0 00005
2 21808 63.3010 325.2588 0885742 73.2996 296.3276 13.59088508 09
| Epoch (UTC): | 13 April 2026 23:00:07 |
| Eccentricity: | 0.0885742 |
| inclination: | 63.3010° |
| perigee height: | 382 km |
| apogee height: | 1696 km |
| right ascension of ascending node: | 325.2588° |
| argument of perigee: | 73.2996° |
| revolutions per day: | 13.59088508 |
| mean anomaly at epoch: | 296.3276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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