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 26106.78011330 +.00000000 +00000-0 +10099-3 0 00008
2 27844 98.6764 116.1074 0009706 11.4859 348.6539 14.24296809 00
| Epoch (UTC): | 16 April 2026 18:43:21 |
| Eccentricity: | 0.0009706 |
| inclination: | 98.6764° |
| perigee height: | 804 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 116.1074° |
| argument of perigee: | 11.4859° |
| revolutions per day: | 14.24296809 |
| mean anomaly at epoch: | 348.6539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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