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 62097U 26145.41663567 +.00000000 +00000-0 +17707-2 0 00007
2 62097 42.9989 300.2918 0001049 229.6271 130.4506 15.70977343 08
| Epoch (UTC): | 25 May 2026 09:59:57 |
| Eccentricity: | 0.0001049 |
| inclination: | 42.9989° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 300.2918° |
| argument of perigee: | 229.6271° |
| revolutions per day: | 15.70977343 |
| mean anomaly at epoch: | 130.4506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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