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 52867U 26145.42024896 +.00000000 +00000-0 +72930-3 0 00008
2 52867 53.2117 39.6637 0001423 105.1654 254.9496 15.08795077 03
| Epoch (UTC): | 25 May 2026 10:05:09 |
| Eccentricity: | 0.0001423 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.6637° |
| argument of perigee: | 105.1654° |
| revolutions per day: | 15.08795077 |
| mean anomaly at epoch: | 254.9496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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