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 55287U 26145.37818860 +.00000000 +00000-0 +32244-4 0 00008
2 55287 69.9986 171.2430 0003972 264.6003 95.4703 14.98333578 05
| Epoch (UTC): | 25 May 2026 09:04:35 |
| Eccentricity: | 0.0003972 |
| inclination: | 69.9986° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 171.2430° |
| argument of perigee: | 264.6003° |
| revolutions per day: | 14.98333578 |
| mean anomaly at epoch: | 95.4703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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