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 26067.00108171 +.00000000 +00000-0 +62977-4 0 00004
2 27387 98.8159 82.7707 0033045 65.6727 294.7903 14.36770791 07
| Epoch (UTC): | 08 March 2026 00:01:33 |
| Eccentricity: | 0.0033045 |
| inclination: | 98.8159° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 82.7707° |
| argument of perigee: | 65.6727° |
| revolutions per day: | 14.36770791 |
| mean anomaly at epoch: | 294.7903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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