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 62495U 26145.21679270 +.00000000 +00000-0 +98739-3 0 00000
2 62495 42.9966 216.9381 0000402 96.1084 263.9814 15.27576011 06
| Epoch (UTC): | 25 May 2026 05:12:10 |
| Eccentricity: | 0.0000402 |
| inclination: | 42.9966° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 216.9381° |
| argument of perigee: | 96.1084° |
| revolutions per day: | 15.27576011 |
| mean anomaly at epoch: | 263.9814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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