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 62307U 26145.47648020 +.00000000 +00000-0 +45130-3 0 00006
2 62307 53.1574 184.2355 0001007 77.4443 282.6670 15.30188655 03
| Epoch (UTC): | 25 May 2026 11:26:07 |
| Eccentricity: | 0.0001007 |
| inclination: | 53.1574° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.2355° |
| argument of perigee: | 77.4443° |
| revolutions per day: | 15.30188655 |
| mean anomaly at epoch: | 282.6670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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