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 64750U 26145.37219429 +.00000000 +00000-0 +65160-3 0 00001
2 64750 53.1598 184.7583 0001045 101.5767 258.5352 15.30211028 01
| Epoch (UTC): | 25 May 2026 08:55:57 |
| Eccentricity: | 0.0001045 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.7583° |
| argument of perigee: | 101.5767° |
| revolutions per day: | 15.30211028 |
| mean anomaly at epoch: | 258.5352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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