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 16012U 26158.69594325 +.00000000 +00000-0 +76423-4 0 00004
2 16012 74.0587 240.1226 0014251 40.3739 319.8470 14.37796560 09
| Epoch (UTC): | 07 June 2026 16:42:09 |
| Eccentricity: | 0.0014251 |
| inclination: | 74.0587° |
| perigee height: | 756 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 240.1226° |
| argument of perigee: | 40.3739° |
| revolutions per day: | 14.37796560 |
| mean anomaly at epoch: | 319.8470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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