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 53069U 26145.49533250 +.00000000 +00000-0 +61062-4 0 00004
2 53069 97.4454 325.3748 0001305 108.2382 251.8987 15.05649989 09
| Epoch (UTC): | 25 May 2026 11:53:16 |
| Eccentricity: | 0.0001305 |
| inclination: | 97.4454° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.3748° |
| argument of perigee: | 108.2382° |
| revolutions per day: | 15.05649989 |
| mean anomaly at epoch: | 251.8987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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