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 27386U 26069.85399071 +.00000000 +00000-0 +70889-4 0 00000
2 27386 98.3729 23.4236 0001318 82.7249 288.7667 14.39037467 09
| Epoch (UTC): | 10 March 2026 20:29:44 |
| Eccentricity: | 0.0001318 |
| inclination: | 98.3729° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 23.4236° |
| argument of perigee: | 82.7249° |
| revolutions per day: | 14.39037467 |
| mean anomaly at epoch: | 288.7667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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