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 23317U 26064.77933432 +.00000000 +00000-0 +27264-3 0 00009
2 23317 82.5378 353.7480 0014574 261.9321 98.0248 14.96859537 04
| Epoch (UTC): | 05 March 2026 18:42:14 |
| Eccentricity: | 0.0014574 |
| inclination: | 82.5378° |
| perigee height: | 566 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 353.7480° |
| argument of perigee: | 261.9321° |
| revolutions per day: | 14.96859537 |
| mean anomaly at epoch: | 98.0248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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