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 26038.98767947 +.00000000 +00000-0 +19968-3 0 00000
2 27844 98.6776 49.1576 0009292 194.6012 165.4899 14.24240500 01
| Epoch (UTC): | 07 February 2026 23:42:15 |
| Eccentricity: | 0.0009292 |
| inclination: | 98.6776° |
| perigee height: | 804 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 49.1576° |
| argument of perigee: | 194.6012° |
| revolutions per day: | 14.24240500 |
| mean anomaly at epoch: | 165.4899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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