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 53207U 26145.44272064 +.00000000 +00000-0 -98863-4 0 00006
2 53207 97.4490 205.3331 0001713 125.9511 234.1876 15.05656573 09
| Epoch (UTC): | 25 May 2026 10:37:31 |
| Eccentricity: | 0.0001713 |
| inclination: | 97.4490° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.3331° |
| argument of perigee: | 125.9511° |
| revolutions per day: | 15.05656573 |
| mean anomaly at epoch: | 234.1876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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