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 53807U 26110.79648043 +.00000000 +00000-0 +71943-4 0 00005
2 53807 53.2296 303.2579 0006253 16.7904 343.3307 15.37597756 02
| Epoch (UTC): | 20 April 2026 19:06:55 |
| Eccentricity: | 0.0006253 |
| inclination: | 53.2296° |
| perigee height: | 449 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 303.2579° |
| argument of perigee: | 16.7904° |
| revolutions per day: | 15.37597756 |
| mean anomaly at epoch: | 343.3307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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