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 62195U 26145.46133222 +.00000000 +00000-0 +71573-3 0 00003
2 62195 43.0018 197.0660 0001368 268.5502 91.5193 15.27582419 08
| Epoch (UTC): | 25 May 2026 11:04:19 |
| Eccentricity: | 0.0001368 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.0660° |
| argument of perigee: | 268.5502° |
| revolutions per day: | 15.27582419 |
| mean anomaly at epoch: | 91.5193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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