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 07009U 26088.23034036 +.00000000 +00000-0 -44012-4 0 00000
2 07009 82.9450 81.8702 0018108 263.1039 108.2101 13.77047126 05
| Epoch (UTC): | 29 March 2026 05:31:41 |
| Eccentricity: | 0.0018108 |
| inclination: | 82.9450° |
| perigee height: | 961 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 81.8702° |
| argument of perigee: | 263.1039° |
| revolutions per day: | 13.77047126 |
| mean anomaly at epoch: | 108.2101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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