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 65083U 26144.96768796 +.00000000 +00000-0 +23905-3 0 00002
2 65083 53.1583 29.8984 0001045 84.2797 275.8322 15.30201172 07
| Epoch (UTC): | 24 May 2026 23:13:28 |
| Eccentricity: | 0.0001045 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.8984° |
| argument of perigee: | 84.2797° |
| revolutions per day: | 15.30201172 |
| mean anomaly at epoch: | 275.8322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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