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 27844U 26288.58002145 +.00000000 +00000-0 +12223-3 0 00002
2 27844 98.6766 295.6480 0009299 189.4555 170.6450 14.24395762 05
| Epoch (UTC): | 15 October 2026 13:55:13 |
| Eccentricity: | 0.0009299 |
| inclination: | 98.6766° |
| perigee height: | 804 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 295.6480° |
| argument of perigee: | 189.4555° |
| revolutions per day: | 14.24395762 |
| mean anomaly at epoch: | 170.6450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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