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 65577U 26145.13114465 +.00000000 +00000-0 +60025-4 0 00003
2 65577 81.3030 31.9725 0006152 253.5240 106.5242 13.84775466 00
| Epoch (UTC): | 25 May 2026 03:08:50 |
| Eccentricity: | 0.0006152 |
| inclination: | 81.3030° |
| perigee height: | 942 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 31.9725° |
| argument of perigee: | 253.5240° |
| revolutions per day: | 13.84775466 |
| mean anomaly at epoch: | 106.5242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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