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 26064.21458921 +.00000000 +00000-0 +50073-3 0 00009
2 21799 63.2957 63.4726 0885340 71.2139 298.2773 13.60205019 06
| Epoch (UTC): | 05 March 2026 05:09:00 |
| Eccentricity: | 0.0885340 |
| inclination: | 63.2957° |
| perigee height: | 379 km |
| apogee height: | 1691 km |
| right ascension of ascending node: | 63.4726° |
| argument of perigee: | 71.2139° |
| revolutions per day: | 13.60205019 |
| mean anomaly at epoch: | 298.2773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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