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 00020U 26040.28003888 +.00000000 +00000-0 +45979-3 0 00001
2 00020 33.3450 7.4400 1638311 87.8661 290.7828 11.61812523 02
| Epoch (UTC): | 09 February 2026 06:43:15 |
| Eccentricity: | 0.1638311 |
| inclination: | 33.3450° |
| perigee height: | 507 km |
| apogee height: | 3206 km |
| right ascension of ascending node: | 7.4400° |
| argument of perigee: | 87.8661° |
| revolutions per day: | 11.61812523 |
| mean anomaly at epoch: | 290.7828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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