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 26075.13817971 +.00000000 +00000-0 +47039-4 0 00003
2 27386 98.3737 28.5823 0001307 82.6749 287.9099 14.39039327 05
| Epoch (UTC): | 16 March 2026 03:18:58 |
| Eccentricity: | 0.0001307 |
| inclination: | 98.3737° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 28.5823° |
| argument of perigee: | 82.6749° |
| revolutions per day: | 14.39039327 |
| mean anomaly at epoch: | 287.9099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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