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 26074.94004741 +.00000000 +00000-0 +46065-4 0 00003
2 27387 98.8154 90.8990 0032805 42.8806 317.4928 14.36773111 03
| Epoch (UTC): | 15 March 2026 22:33:40 |
| Eccentricity: | 0.0032805 |
| inclination: | 98.8154° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 90.8990° |
| argument of perigee: | 42.8806° |
| revolutions per day: | 14.36773111 |
| mean anomaly at epoch: | 317.4928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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