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 45568U 26145.89105556 +.00000000 +00000-0 +68534-3 0 00007
2 45568 53.0281 4.5315 0007283 258.1574 101.8644 16.11724683 02
| Epoch (UTC): | 25 May 2026 21:23:07 |
| Eccentricity: | 0.0007283 |
| inclination: | 53.0281° |
| perigee height: | 237 km |
| apogee height: | 247 km |
| right ascension of ascending node: | 4.5315° |
| argument of perigee: | 258.1574° |
| revolutions per day: | 16.11724683 |
| mean anomaly at epoch: | 101.8644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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