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 62035U 26145.47252409 +.00000000 +00000-0 +33175-3 0 00002
2 62035 42.9999 190.0398 0001549 281.7078 78.3600 15.27603665 07
| Epoch (UTC): | 25 May 2026 11:20:26 |
| Eccentricity: | 0.0001549 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 190.0398° |
| argument of perigee: | 281.7078° |
| revolutions per day: | 15.27603665 |
| mean anomaly at epoch: | 78.3600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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