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 52345U 26145.44742433 +.00000000 +00000-0 +62049-4 0 00006
2 52345 53.2139 214.7080 0001194 91.3082 268.8047 15.08839214 00
| Epoch (UTC): | 25 May 2026 10:44:17 |
| Eccentricity: | 0.0001194 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.7080° |
| argument of perigee: | 91.3082° |
| revolutions per day: | 15.08839214 |
| mean anomaly at epoch: | 268.8047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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