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 27380U 26108.28804524 +.00000000 +00000-0 +00000-0 0 00003
2 27380 6.7714 69.8866 0007363 333.6028 235.1546 1.00271284 05
| Epoch (UTC): | 18 April 2026 06:54:47 |
| Eccentricity: | 0.0007363 |
| inclination: | 6.7714° |
| perigee height: | 35756 km |
| apogee height: | 35818 km |
| right ascension of ascending node: | 69.8866° |
| argument of perigee: | 333.6028° |
| revolutions per day: | 1.00271284 |
| mean anomaly at epoch: | 235.1546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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