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 26071.47222045 +.00000000 +00000-0 +68716-4 0 00003
2 27386 98.3732 25.0034 0001309 83.1199 26.8150 14.39038169 04
| Epoch (UTC): | 12 March 2026 11:19:59 |
| Eccentricity: | 0.0001309 |
| inclination: | 98.3732° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 25.0034° |
| argument of perigee: | 83.1199° |
| revolutions per day: | 14.39038169 |
| mean anomaly at epoch: | 26.8150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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