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 26069.50812603 +.00000000 +00000-0 +52747-4 0 00007
2 27387 98.8157 85.3375 0032985 58.4993 301.9408 14.36771493 03
| Epoch (UTC): | 10 March 2026 12:11:42 |
| Eccentricity: | 0.0032985 |
| inclination: | 98.8157° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 85.3375° |
| argument of perigee: | 58.4993° |
| revolutions per day: | 14.36771493 |
| mean anomaly at epoch: | 301.9408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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