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 52312U 26145.29463888 +.00000000 +00000-0 +67872-4 0 00006
2 52312 53.2148 105.1761 0001291 80.7147 279.3991 15.08839458 00
| Epoch (UTC): | 25 May 2026 07:04:16 |
| Eccentricity: | 0.0001291 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.1761° |
| argument of perigee: | 80.7147° |
| revolutions per day: | 15.08839458 |
| mean anomaly at epoch: | 279.3991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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