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 65022U 26145.41465387 +.00000000 +00000-0 +65666-3 0 00006
2 65022 53.1586 298.0447 0001656 101.8377 258.2810 15.30217761 03
| Epoch (UTC): | 25 May 2026 09:57:06 |
| Eccentricity: | 0.0001656 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 298.0447° |
| argument of perigee: | 101.8377° |
| revolutions per day: | 15.30217761 |
| mean anomaly at epoch: | 258.2810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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