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 16953U 26156.87533670 +.00000000 +00000-0 +75581-4 0 00006
2 16953 74.0119 356.9547 0011830 161.5680 198.5906 14.38862664 03
| Epoch (UTC): | 05 June 2026 21:00:29 |
| Eccentricity: | 0.0011830 |
| inclination: | 74.0119° |
| perigee height: | 754 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 356.9547° |
| argument of perigee: | 161.5680° |
| revolutions per day: | 14.38862664 |
| mean anomaly at epoch: | 198.5906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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