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 27387U 26042.06978410 +.00000000 +00000-0 +48085-4 0 00008
2 27387 98.8166 57.2450 0032831 137.0612 223.3145 14.36763493 03
| Epoch (UTC): | 11 February 2026 01:40:29 |
| Eccentricity: | 0.0032831 |
| inclination: | 98.8166° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 57.2450° |
| argument of perigee: | 137.0612° |
| revolutions per day: | 14.36763493 |
| mean anomaly at epoch: | 223.3145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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