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 53070U 26145.22256455 +.00000000 +00000-0 +61282-3 0 00009
2 53070 97.4475 326.3616 0001368 89.7438 270.3946 15.05604184 02
| Epoch (UTC): | 25 May 2026 05:20:29 |
| Eccentricity: | 0.0001368 |
| inclination: | 97.4475° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.3616° |
| argument of perigee: | 89.7438° |
| revolutions per day: | 15.05604184 |
| mean anomaly at epoch: | 270.3946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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