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 62420U 26145.47071306 +.00000000 +00000-0 +13416-2 0 00000
2 62420 42.9977 65.0755 0002579 285.1605 74.8978 15.70908572 09
| Epoch (UTC): | 25 May 2026 11:17:49 |
| Eccentricity: | 0.0002579 |
| inclination: | 42.9977° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 65.0755° |
| argument of perigee: | 285.1605° |
| revolutions per day: | 15.70908572 |
| mean anomaly at epoch: | 74.8978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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