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 26044.60788670 +.00000000 +00000-0 +17910-3 0 00007
2 27844 98.6776 54.7070 0009582 178.0211 182.1008 14.24245361 09
| Epoch (UTC): | 13 February 2026 14:35:21 |
| Eccentricity: | 0.0009582 |
| inclination: | 98.6776° |
| perigee height: | 804 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 54.7070° |
| argument of perigee: | 178.0211° |
| revolutions per day: | 14.24245361 |
| mean anomaly at epoch: | 182.1008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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