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 53278U 26145.52694573 +.00000000 +00000-0 -89442-4 0 00009
2 53278 53.2112 199.1824 0000713 114.5653 245.5414 15.08839470 01
| Epoch (UTC): | 25 May 2026 12:38:48 |
| Eccentricity: | 0.0000713 |
| inclination: | 53.2112° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 199.1824° |
| argument of perigee: | 114.5653° |
| revolutions per day: | 15.08839470 |
| mean anomaly at epoch: | 245.5414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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