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 62740U 26145.52334154 +.00000000 +00000-0 +86889-3 0 00009
2 62740 43.0019 80.8628 0000728 266.8977 93.1791 15.27590103 05
| Epoch (UTC): | 25 May 2026 12:33:36 |
| Eccentricity: | 0.0000728 |
| inclination: | 43.0019° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.8628° |
| argument of perigee: | 266.8977° |
| revolutions per day: | 15.27590103 |
| mean anomaly at epoch: | 93.1791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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