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 64865U 26145.13631512 +.00000000 +00000-0 +22027-3 0 00008
2 64865 97.4501 0.5279 0001854 79.7920 280.3516 15.05650982 08
| Epoch (UTC): | 25 May 2026 03:16:17 |
| Eccentricity: | 0.0001854 |
| inclination: | 97.4501° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.5279° |
| argument of perigee: | 79.7920° |
| revolutions per day: | 15.05650982 |
| mean anomaly at epoch: | 280.3516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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