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 45179U 26145.58335647 +.00000000 +00000-0 +50450-3 0 00005
2 45179 53.0368 307.9681 0003824 309.9427 117.4447 15.84104094 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003824 |
| inclination: | 53.0368° |
| perigee height: | 316 km |
| apogee height: | 321 km |
| right ascension of ascending node: | 307.9681° |
| argument of perigee: | 309.9427° |
| revolutions per day: | 15.84104094 |
| mean anomaly at epoch: | 117.4447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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