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 53208U 26145.43991869 +.00000000 +00000-0 +31285-3 0 00000
2 53208 97.4511 205.3612 0001862 134.3331 225.8049 15.05693574 06
| Epoch (UTC): | 25 May 2026 10:33:28 |
| Eccentricity: | 0.0001862 |
| inclination: | 97.4511° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.3612° |
| argument of perigee: | 134.3331° |
| revolutions per day: | 15.05693574 |
| mean anomaly at epoch: | 225.8049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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