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 26067.62784302 +.00000000 +00000-0 +61278-4 0 00001
2 27387 98.8159 83.4124 0033039 63.8815 296.5764 14.36770979 02
| Epoch (UTC): | 08 March 2026 15:04:05 |
| Eccentricity: | 0.0033039 |
| inclination: | 98.8159° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 83.4124° |
| argument of perigee: | 63.8815° |
| revolutions per day: | 14.36770979 |
| mean anomaly at epoch: | 296.5764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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