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 23752U 26088.16593316 +.00000000 +00000-0 +26598-4 0 00004
2 23752 98.7403 160.0580 0005495 9.5082 350.6201 14.26148229 05
| Epoch (UTC): | 29 March 2026 03:58:56 |
| Eccentricity: | 0.0005495 |
| inclination: | 98.7403° |
| perigee height: | 801 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 160.0580° |
| argument of perigee: | 9.5082° |
| revolutions per day: | 14.26148229 |
| mean anomaly at epoch: | 350.6201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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