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 65038U 26144.64765902 +.00000000 +00000-0 +12124-2 0 00003
2 65038 53.1594 301.0767 0001067 94.1716 265.9407 15.30201174 04
| Epoch (UTC): | 24 May 2026 15:32:37 |
| Eccentricity: | 0.0001067 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 301.0767° |
| argument of perigee: | 94.1716° |
| revolutions per day: | 15.30201174 |
| mean anomaly at epoch: | 265.9407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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