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 21797U 26017.92894470 +.00000000 +00000-0 +55890-4 0 00009
2 21797 82.9514 252.0018 0036873 298.9927 71.6239 13.77863633 03
| Epoch (UTC): | 17 January 2026 22:17:40 |
| Eccentricity: | 0.0036873 |
| inclination: | 82.9514° |
| perigee height: | 944 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 252.0018° |
| argument of perigee: | 298.9927° |
| revolutions per day: | 13.77863633 |
| mean anomaly at epoch: | 71.6239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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