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 21799U 26135.27573616 +.00000000 +00000-0 +17906-3 0 00001
2 21799 63.2956 232.3959 0882994 72.6048 296.9511 13.61248857 09
| Epoch (UTC): | 15 May 2026 06:37:03 |
| Eccentricity: | 0.0882994 |
| inclination: | 63.2956° |
| perigee height: | 377 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 232.3959° |
| argument of perigee: | 72.6048° |
| revolutions per day: | 13.61248857 |
| mean anomaly at epoch: | 296.9511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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