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 26111.85128999 +.00000000 +00000-0 +24179-3 0 00008
2 40012 97.7809 265.5903 0044020 253.5405 106.0972 14.87904891 09
| Epoch (UTC): | 21 April 2026 20:25:51 |
| Eccentricity: | 0.0044020 |
| inclination: | 97.7809° |
| perigee height: | 574 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 265.5903° |
| argument of perigee: | 253.5405° |
| revolutions per day: | 14.87904891 |
| mean anomaly at epoch: | 106.0972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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