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 26106.25461815 +.00000000 +00000-0 +20968-4 0 00002
2 27004 99.8052 281.9514 0019153 302.8157 240.1056 13.70259841 01
| Epoch (UTC): | 16 April 2026 06:06:39 |
| Eccentricity: | 0.0019153 |
| inclination: | 99.8052° |
| perigee height: | 985 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 281.9514° |
| argument of perigee: | 302.8157° |
| revolutions per day: | 13.70259841 |
| mean anomaly at epoch: | 240.1056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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