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 26062.86550994 +.00000000 +00000-0 +00000-0 0 00005
2 27380 6.6574 70.4474 0006109 305.4536 65.8068 1.00273362 05
| Epoch (UTC): | 03 March 2026 20:46:20 |
| Eccentricity: | 0.0006109 |
| inclination: | 6.6574° |
| perigee height: | 35760 km |
| apogee height: | 35812 km |
| right ascension of ascending node: | 70.4474° |
| argument of perigee: | 305.4536° |
| revolutions per day: | 1.00273362 |
| mean anomaly at epoch: | 65.8068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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