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 62036U 26145.45293462 +.00000000 +00000-0 +43538-3 0 00009
2 62036 42.9992 182.9722 0001453 272.0914 87.9771 15.27593915 09
| Epoch (UTC): | 25 May 2026 10:52:13 |
| Eccentricity: | 0.0001453 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.9722° |
| argument of perigee: | 272.0914° |
| revolutions per day: | 15.27593915 |
| mean anomaly at epoch: | 87.9771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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