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 data is extracted from the following two-line orbital elements,
1 27846U 03031G 25138.91406476 .00000304 00000-0 15263-3 0 9997
2 27846 98.6867 147.1315 0008428 220.6008 139.4543 14.23675786135585
| Epoch (UTC): | 18 May 2025 21:56:15 |
| Eccentricity: | 0.0008428 |
| inclination: | 98.6867° |
| perigee height: | 807 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 147.1315° |
| argument of perigee: | 220.6008° |
| revolutions per day: | 14.23675786 |
| mean anomaly at epoch: | 139.4543° |
| orbit number at epoch: | 13558 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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