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 10096U 26016.87252414 +.00000000 +00000-0 +63201-4 0 00003
2 10096 75.8319 182.9232 0040430 130.2389 230.2352 14.91911031 02
| Epoch (UTC): | 16 January 2026 20:56:26 |
| Eccentricity: | 0.0040430 |
| inclination: | 75.8319° |
| perigee height: | 564 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 182.9232° |
| argument of perigee: | 130.2389° |
| revolutions per day: | 14.91911031 |
| mean anomaly at epoch: | 230.2352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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