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 62085U 26145.57581556 +.00000000 +00000-0 +13471-3 0 00003
2 62085 98.0046 309.5455 0001903 30.1711 329.9609 14.78273730 07
| Epoch (UTC): | 25 May 2026 13:49:10 |
| Eccentricity: | 0.0001903 |
| inclination: | 98.0046° |
| perigee height: | 633 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 309.5455° |
| argument of perigee: | 30.1711° |
| revolutions per day: | 14.78273730 |
| mean anomaly at epoch: | 329.9609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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