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 26106.28836476 +.00000000 +00000-0 +10234-3 0 00000
2 27844 98.6764 115.6217 0009738 12.8903 347.2523 14.24296578 04
| Epoch (UTC): | 16 April 2026 06:55:14 |
| Eccentricity: | 0.0009738 |
| inclination: | 98.6764° |
| perigee height: | 804 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 115.6217° |
| argument of perigee: | 12.8903° |
| revolutions per day: | 14.24296578 |
| mean anomaly at epoch: | 347.2523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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