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 26959U 01049C 23284.08619489 .06935024 27864-5 38094-3 0 9997
2 26959 97.7693 66.3671 0010118 271.3565 88.6575 16.41532284528148
| Epoch (UTC): | 11 October 2023 02:04:07 |
| Eccentricity: | 0.0010118 |
| inclination: | 97.7693° |
| perigee height: | 155 km |
| apogee height: | 168 km |
| right ascension of ascending node: | 66.3671° |
| argument of perigee: | 271.3565° |
| revolutions per day: | 16.41532284 |
| mean anomaly at epoch: | 88.6575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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