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 26037.62598501 +.00000000 +00000-0 +12082-3 0 00003
2 16012 74.0579 102.7194 0016106 295.0576 64.8905 14.37733658 05
| Epoch (UTC): | 06 February 2026 15:01:25 |
| Eccentricity: | 0.0016106 |
| inclination: | 74.0579° |
| perigee height: | 754 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 102.7194° |
| argument of perigee: | 295.0576° |
| revolutions per day: | 14.37733658 |
| mean anomaly at epoch: | 64.8905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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