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 52699U 26145.34524723 +.00000000 +00000-0 -44048-3 0 00006
2 52699 53.2108 155.0311 0001296 95.5144 264.5996 15.08875711 08
| Epoch (UTC): | 25 May 2026 08:17:09 |
| Eccentricity: | 0.0001296 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 155.0311° |
| argument of perigee: | 95.5144° |
| revolutions per day: | 15.08875711 |
| mean anomaly at epoch: | 264.5996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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