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 53074U 26145.48106965 +.00000000 +00000-0 -68149-5 0 00003
2 53074 97.5786 326.8854 0001277 99.4982 260.6391 15.08343125 06
| Epoch (UTC): | 25 May 2026 11:32:44 |
| Eccentricity: | 0.0001277 |
| inclination: | 97.5786° |
| perigee height: | 540 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 326.8854° |
| argument of perigee: | 99.4982° |
| revolutions per day: | 15.08343125 |
| mean anomaly at epoch: | 260.6391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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