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 65499U 26145.35618910 +.00000000 +00000-0 +62907-3 0 00004
2 65499 53.1596 275.2008 0001272 78.3376 281.7767 15.30207794 00
| Epoch (UTC): | 25 May 2026 08:32:54 |
| Eccentricity: | 0.0001272 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 275.2008° |
| argument of perigee: | 78.3376° |
| revolutions per day: | 15.30207794 |
| mean anomaly at epoch: | 281.7767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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