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 65029U 26145.42313653 +.00000000 +00000-0 +10933-2 0 00008
2 65029 53.1613 297.3890 0001524 103.6702 256.4470 15.34407715 07
| Epoch (UTC): | 25 May 2026 10:09:18 |
| Eccentricity: | 0.0001524 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 297.3890° |
| argument of perigee: | 103.6702° |
| revolutions per day: | 15.34407715 |
| mean anomaly at epoch: | 256.4470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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