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 26040.95553106 +.00000000 +00000-0 +47934-4 0 00007
2 27387 98.8166 56.1043 0032782 140.2802 220.0793 14.36763159 03
| Epoch (UTC): | 09 February 2026 22:55:57 |
| Eccentricity: | 0.0032782 |
| inclination: | 98.8166° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 56.1043° |
| argument of perigee: | 140.2802° |
| revolutions per day: | 14.36763159 |
| mean anomaly at epoch: | 220.0793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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