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 65081U 26144.95396935 +.00000000 +00000-0 +52955-3 0 00008
2 65081 53.1604 29.8113 0001117 87.9600 272.1529 15.30204693 06
| Epoch (UTC): | 24 May 2026 22:53:42 |
| Eccentricity: | 0.0001117 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.8113° |
| argument of perigee: | 87.9600° |
| revolutions per day: | 15.30204693 |
| mean anomaly at epoch: | 272.1529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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