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 40012U 26106.67299772 +.00000000 +00000-0 +18787-3 0 00008
2 40012 97.7800 260.5098 0043957 271.1218 88.4963 14.87884173 09
| Epoch (UTC): | 16 April 2026 16:09:07 |
| Eccentricity: | 0.0043957 |
| inclination: | 97.7800° |
| perigee height: | 574 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 260.5098° |
| argument of perigee: | 271.1218° |
| revolutions per day: | 14.87884173 |
| mean anomaly at epoch: | 88.4963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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