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 08473U 26087.73984196 +.00000000 +00000-0 +12435-4 0 00004
2 08473 65.0777 202.6210 0089347 317.7326 41.6870 13.82324222 04
| Epoch (UTC): | 28 March 2026 17:45:22 |
| Eccentricity: | 0.0089347 |
| inclination: | 65.0777° |
| perigee height: | 890 km |
| apogee height: | 1021 km |
| right ascension of ascending node: | 202.6210° |
| argument of perigee: | 317.7326° |
| revolutions per day: | 13.82324222 |
| mean anomaly at epoch: | 41.6870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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