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 22285U 26156.51132367 +.00000000 +00000-0 +20745-4 0 00002
2 22285 71.0203 179.9023 0004582 203.9491 156.1420 14.15464970 02
| Epoch (UTC): | 05 June 2026 12:16:18 |
| Eccentricity: | 0.0004582 |
| inclination: | 71.0203° |
| perigee height: | 837 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 179.9023° |
| argument of perigee: | 203.9491° |
| revolutions per day: | 14.15464970 |
| mean anomaly at epoch: | 156.1420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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