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 53807U 26160.44790487 +.00000000 +00000-0 +14746-3 0 00009
2 53807 53.2293 70.3023 0006885 138.9508 221.2017 15.38173453 00
| Epoch (UTC): | 09 June 2026 10:44:58 |
| Eccentricity: | 0.0006885 |
| inclination: | 53.2293° |
| perigee height: | 447 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 70.3023° |
| argument of perigee: | 138.9508° |
| revolutions per day: | 15.38173453 |
| mean anomaly at epoch: | 221.2017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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