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 27945U 26104.16984616 +.00000000 +00000-0 +49770-4 0 00005
2 27945 98.3784 271.4399 0011583 172.9901 187.1467 14.67834198 05
| Epoch (UTC): | 14 April 2026 04:04:34 |
| Eccentricity: | 0.0011583 |
| inclination: | 98.3784° |
| perigee height: | 660 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 271.4399° |
| argument of perigee: | 172.9901° |
| revolutions per day: | 14.67834198 |
| mean anomaly at epoch: | 187.1467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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