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 26073.12175975 +.00000000 +00000-0 +59243-4 0 00001
2 27386 98.3735 26.6137 0001314 83.1274 287.3603 14.39038718 05
| Epoch (UTC): | 14 March 2026 02:55:20 |
| Eccentricity: | 0.0001314 |
| inclination: | 98.3735° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 26.6137° |
| argument of perigee: | 83.1274° |
| revolutions per day: | 14.39038718 |
| mean anomaly at epoch: | 287.3603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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