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 65259U 26139.74599858 +.00000000 +00000-0 +44106-3 0 00004
2 65259 97.5163 268.5846 0013141 61.5305 298.7253 15.22188793 01
| Epoch (UTC): | 19 May 2026 17:54:14 |
| Eccentricity: | 0.0013141 |
| inclination: | 97.5163° |
| perigee height: | 490 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 268.5846° |
| argument of perigee: | 61.5305° |
| revolutions per day: | 15.22188793 |
| mean anomaly at epoch: | 298.7253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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