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 27004U 26106.98117515 +.00000000 +00000-0 +18645-4 0 00006
2 27004 99.8053 282.6915 0019141 300.8813 224.2391 13.70259892 00
| Epoch (UTC): | 16 April 2026 23:32:53 |
| Eccentricity: | 0.0019141 |
| inclination: | 99.8053° |
| perigee height: | 985 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 282.6915° |
| argument of perigee: | 300.8813° |
| revolutions per day: | 13.70259892 |
| mean anomaly at epoch: | 224.2391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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