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 62090U 26145.45380132 +.00000000 +00000-0 +16562-2 0 00006
2 62090 42.9989 300.5908 0002144 274.4438 85.6185 15.70897872 05
| Epoch (UTC): | 25 May 2026 10:53:28 |
| Eccentricity: | 0.0002144 |
| inclination: | 42.9989° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 300.5908° |
| argument of perigee: | 274.4438° |
| revolutions per day: | 15.70897872 |
| mean anomaly at epoch: | 85.6185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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