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 27002U 26050.46350001 +.00000000 +00000-0 +58126-4 0 00002
2 27002 99.7851 223.1317 0020146 76.9351 301.8484 13.70626821 09
| Epoch (UTC): | 19 February 2026 11:07:26 |
| Eccentricity: | 0.0020146 |
| inclination: | 99.7851° |
| perigee height: | 982 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 223.1317° |
| argument of perigee: | 76.9351° |
| revolutions per day: | 13.70626821 |
| mean anomaly at epoch: | 301.8484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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