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 27845U 26150.81580889 +.00000000 +00000-0 +22547-3 0 00003
2 27845 98.6628 159.8361 0007348 251.2510 108.7873 14.24934161 07
| Epoch (UTC): | 30 May 2026 19:34:45 |
| Eccentricity: | 0.0007348 |
| inclination: | 98.6628° |
| perigee height: | 803 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 159.8361° |
| argument of perigee: | 251.2510° |
| revolutions per day: | 14.24934161 |
| mean anomaly at epoch: | 108.7873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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