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 65031U 26145.41782448 +.00000000 +00000-0 +52744-3 0 00009
2 65031 53.1604 298.0653 0001127 84.8585 275.2544 15.30205838 02
| Epoch (UTC): | 25 May 2026 10:01:40 |
| Eccentricity: | 0.0001127 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 298.0653° |
| argument of perigee: | 84.8585° |
| revolutions per day: | 15.30205838 |
| mean anomaly at epoch: | 275.2544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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