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 27847U 26053.78248125 +.00000000 +00000-0 +12310-3 0 00004
2 27847 98.6903 63.6063 0010062 131.9937 228.2100 14.23791097 09
| Epoch (UTC): | 22 February 2026 18:46:46 |
| Eccentricity: | 0.0010062 |
| inclination: | 98.6903° |
| perigee height: | 805 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 63.6063° |
| argument of perigee: | 131.9937° |
| revolutions per day: | 14.23791097 |
| mean anomaly at epoch: | 228.2100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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