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 26145.44054367 +.00000000 +00000-0 +34521-4 0 00006
2 27004 99.8074 321.8723 0019569 199.0689 225.2973 13.70261394 06
| Epoch (UTC): | 25 May 2026 10:34:22 |
| Eccentricity: | 0.0019569 |
| inclination: | 99.8074° |
| perigee height: | 984 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 321.8723° |
| argument of perigee: | 199.0689° |
| revolutions per day: | 13.70261394 |
| mean anomaly at epoch: | 225.2973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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