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 62136U 26145.15116582 +.00000000 +00000-0 +87102-3 0 00009
2 62136 43.0017 64.2934 0001248 252.4199 107.6516 15.27588847 01
| Epoch (UTC): | 25 May 2026 03:37:40 |
| Eccentricity: | 0.0001248 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.2934° |
| argument of perigee: | 252.4199° |
| revolutions per day: | 15.27588847 |
| mean anomaly at epoch: | 107.6516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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