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 26044.92186287 +.00000000 +00000-0 +38076-3 0 00001
2 00020 33.3449 350.7322 1638244 112.7472 265.4182 11.61821940 05
| Epoch (UTC): | 13 February 2026 22:07:28 |
| Eccentricity: | 0.1638244 |
| inclination: | 33.3449° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 350.7322° |
| argument of perigee: | 112.7472° |
| revolutions per day: | 11.61821940 |
| mean anomaly at epoch: | 265.4182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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