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 63865U 26145.13674108 +.00000000 +00000-0 +30348-3 0 00000
2 63865 70.0023 41.7334 0002849 268.9456 91.1376 14.98338529 06
| Epoch (UTC): | 25 May 2026 03:16:54 |
| Eccentricity: | 0.0002849 |
| inclination: | 70.0023° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.7334° |
| argument of perigee: | 268.9456° |
| revolutions per day: | 14.98338529 |
| mean anomaly at epoch: | 91.1376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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