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 26160.10117362 +.00000000 +00000-0 +58551-4 0 00003
2 10096 75.8333 287.1113 0040113 123.0610 237.4445 14.92126075 08
| Epoch (UTC): | 09 June 2026 02:25:41 |
| Eccentricity: | 0.0040113 |
| inclination: | 75.8333° |
| perigee height: | 563 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 287.1113° |
| argument of perigee: | 123.0610° |
| revolutions per day: | 14.92126075 |
| mean anomaly at epoch: | 237.4445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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