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 53806U 26145.36086875 +.00000000 +00000-0 +20785-4 0 00002
2 53806 53.2140 264.7734 0001216 91.5749 268.5382 15.08837247 06
| Epoch (UTC): | 25 May 2026 08:39:39 |
| Eccentricity: | 0.0001216 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 264.7734° |
| argument of perigee: | 91.5749° |
| revolutions per day: | 15.08837247 |
| mean anomaly at epoch: | 268.5382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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