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 23814U 26088.15625184 +.00000000 +00000-0 +69883-4 0 00005
2 23814 90.0165 341.1409 0023718 48.2059 312.1155 14.25342068 05
| Epoch (UTC): | 29 March 2026 03:45:00 |
| Eccentricity: | 0.0023718 |
| inclination: | 90.0165° |
| perigee height: | 790 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 341.1409° |
| argument of perigee: | 48.2059° |
| revolutions per day: | 14.25342068 |
| mean anomaly at epoch: | 312.1155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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