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 53827U 26145.48280382 +.00000000 +00000-0 -36034-4 0 00002
2 53827 53.2147 319.4441 0000865 87.0224 273.0867 15.08827662 05
| Epoch (UTC): | 25 May 2026 11:35:14 |
| Eccentricity: | 0.0000865 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 319.4441° |
| argument of perigee: | 87.0224° |
| revolutions per day: | 15.08827662 |
| mean anomaly at epoch: | 273.0867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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