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 53258U 26145.45978669 +.00000000 +00000-0 -14708-4 0 00003
2 53258 53.2107 209.4862 0001195 85.4329 274.6800 15.08839304 09
| Epoch (UTC): | 25 May 2026 11:02:05 |
| Eccentricity: | 0.0001195 |
| inclination: | 53.2107° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 209.4862° |
| argument of perigee: | 85.4329° |
| revolutions per day: | 15.08839304 |
| mean anomaly at epoch: | 274.6800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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