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 62132U 26145.19083985 +.00000000 +00000-0 +78183-3 0 00008
2 62132 42.9996 63.7298 0001112 278.8130 81.2596 15.27598243 01
| Epoch (UTC): | 25 May 2026 04:34:48 |
| Eccentricity: | 0.0001112 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 63.7298° |
| argument of perigee: | 278.8130° |
| revolutions per day: | 15.27598243 |
| mean anomaly at epoch: | 81.2596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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