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 62958U 26145.50463189 +.00000000 +00000-0 +57747-3 0 00000
2 62958 53.1603 233.1503 0000752 355.0574 5.0421 15.34396835 09
| Epoch (UTC): | 25 May 2026 12:06:40 |
| Eccentricity: | 0.0000752 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 233.1503° |
| argument of perigee: | 355.0574° |
| revolutions per day: | 15.34396835 |
| mean anomaly at epoch: | 5.0421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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