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 65383U 26145.37428294 +.00000000 +00000-0 +18041-3 0 00002
2 65383 97.4510 16.6609 0002087 76.5531 283.5928 15.05657436 04
| Epoch (UTC): | 25 May 2026 08:58:58 |
| Eccentricity: | 0.0002087 |
| inclination: | 97.4510° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.6609° |
| argument of perigee: | 76.5531° |
| revolutions per day: | 15.05657436 |
| mean anomaly at epoch: | 283.5928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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