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 26103.26492426 +.00000000 +00000-0 +36169-4 0 00005
2 21797 82.9567 188.5787 0039053 60.0315 4.7969 13.77869681 05
| Epoch (UTC): | 13 April 2026 06:21:29 |
| Eccentricity: | 0.0039053 |
| inclination: | 82.9567° |
| perigee height: | 943 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 188.5787° |
| argument of perigee: | 60.0315° |
| revolutions per day: | 13.77869681 |
| mean anomaly at epoch: | 4.7969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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