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 26153.89549882 +.00000000 +00000-0 +00000-0 0 00003
2 27380 6.8847 69.3551 0007343 357.6577 115.2464 1.00271292 08
| Epoch (UTC): | 02 June 2026 21:29:31 |
| Eccentricity: | 0.0007343 |
| inclination: | 6.8847° |
| perigee height: | 35756 km |
| apogee height: | 35818 km |
| right ascension of ascending node: | 69.3551° |
| argument of perigee: | 357.6577° |
| revolutions per day: | 1.00271292 |
| mean anomaly at epoch: | 115.2464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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