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 24967U 26088.14838770 +.00000000 +00000-0 +13917-3 0 00007
2 24967 86.3948 53.1972 0002191 94.5324 265.6124 14.37889166 04
| Epoch (UTC): | 29 March 2026 03:33:40 |
| Eccentricity: | 0.0002191 |
| inclination: | 86.3948° |
| perigee height: | 764 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 53.1972° |
| argument of perigee: | 94.5324° |
| revolutions per day: | 14.37889166 |
| mean anomaly at epoch: | 265.6124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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