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 26156.81569131 +.00000000 +00000-0 +79945-4 0 00001
2 10096 75.8333 292.9804 0040192 131.5938 228.8711 14.92122140 02
| Epoch (UTC): | 05 June 2026 19:34:35 |
| Eccentricity: | 0.0040192 |
| inclination: | 75.8333° |
| perigee height: | 563 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 292.9804° |
| argument of perigee: | 131.5938° |
| revolutions per day: | 14.92122140 |
| mean anomaly at epoch: | 228.8711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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