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 26067.76921938 +.00000000 +00000-0 +91749-4 0 00009
2 10096 75.8307 92.0350 0040966 357.8940 2.2073 14.92006219 06
| Epoch (UTC): | 08 March 2026 18:27:40 |
| Eccentricity: | 0.0040966 |
| inclination: | 75.8307° |
| perigee height: | 563 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 92.0350° |
| argument of perigee: | 357.8940° |
| revolutions per day: | 14.92006219 |
| mean anomaly at epoch: | 2.2073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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