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 17304U 26041.98303750 +.00000000 +00000-0 +11421-3 0 00008
2 17304 74.0569 37.2576 0028708 167.1389 193.0505 14.39128598 01
| Epoch (UTC): | 10 February 2026 23:35:34 |
| Eccentricity: | 0.0028708 |
| inclination: | 74.0569° |
| perigee height: | 741 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 37.2576° |
| argument of perigee: | 167.1389° |
| revolutions per day: | 14.39128598 |
| mean anomaly at epoch: | 193.0505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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