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 27540U 26076.29024492 +.00000000 +00000-0 +00000-0 0 00004
2 27540 90.5446 351.6701 8669856 263.0375 348.4669 0.37586252 03
| Epoch (UTC): | 17 March 2026 06:57:57 |
| Eccentricity: | 0.8669856 |
| inclination: | 90.5446° |
| perigee height: | 4410 km |
| apogee height: | 145044 km |
| right ascension of ascending node: | 351.6701° |
| argument of perigee: | 263.0375° |
| revolutions per day: | 0.37586252 |
| mean anomaly at epoch: | 348.4669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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