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 62215U 26145.48315205 +.00000000 +00000-0 +53045-3 0 00005
2 62215 42.9987 197.2157 0001954 266.2563 93.8066 15.27591506 01
| Epoch (UTC): | 25 May 2026 11:35:44 |
| Eccentricity: | 0.0001954 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.2157° |
| argument of perigee: | 266.2563° |
| revolutions per day: | 15.27591506 |
| mean anomaly at epoch: | 93.8066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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