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 62665U 26145.63680155 +.00000000 +00000-0 +15659-3 0 00009
2 62665 97.3891 224.5111 0005390 65.0092 295.1704 15.22158825 06
| Epoch (UTC): | 25 May 2026 15:16:59 |
| Eccentricity: | 0.0005390 |
| inclination: | 97.3891° |
| perigee height: | 496 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 224.5111° |
| argument of perigee: | 65.0092° |
| revolutions per day: | 15.22158825 |
| mean anomaly at epoch: | 295.1704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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