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 53060U 26145.45659240 +.00000000 +00000-0 -22404-3 0 00006
2 53060 97.4506 325.3197 0001554 63.8689 296.2698 15.05632058 09
| Epoch (UTC): | 25 May 2026 10:57:29 |
| Eccentricity: | 0.0001554 |
| inclination: | 97.4506° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 325.3197° |
| argument of perigee: | 63.8689° |
| revolutions per day: | 15.05632058 |
| mean anomaly at epoch: | 296.2698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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