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 52858U 26145.39815153 +.00000000 +00000-0 +10028-4 0 00009
2 52858 53.2136 39.7901 0001422 89.5273 270.5882 15.08836500 00
| Epoch (UTC): | 25 May 2026 09:33:20 |
| Eccentricity: | 0.0001422 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.7901° |
| argument of perigee: | 89.5273° |
| revolutions per day: | 15.08836500 |
| mean anomaly at epoch: | 270.5882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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