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 65018U 26145.58335647 +.00000000 +00000-0 -59757-3 0 00009
2 65018 53.1601 297.3577 0001239 89.0445 74.3608 15.30201278 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001239 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 297.3577° |
| argument of perigee: | 89.0445° |
| revolutions per day: | 15.30201278 |
| mean anomaly at epoch: | 74.3608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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