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 65277U 26145.57917497 +.00000000 +00000-0 +13575-3 0 00001
2 65277 97.4500 198.1239 0002183 142.4810 217.6570 15.05655230 01
| Epoch (UTC): | 25 May 2026 13:54:00 |
| Eccentricity: | 0.0002183 |
| inclination: | 97.4500° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 198.1239° |
| argument of perigee: | 142.4810° |
| revolutions per day: | 15.05655230 |
| mean anomaly at epoch: | 217.6570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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