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 53253U 26145.60330736 +.00000000 +00000-0 -87419-5 0 00002
2 53253 53.2146 208.8418 0001025 82.8436 277.2672 15.08838920 08
| Epoch (UTC): | 25 May 2026 14:28:45 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 208.8418° |
| argument of perigee: | 82.8436° |
| revolutions per day: | 15.08838920 |
| mean anomaly at epoch: | 277.2672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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