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 36869U 26160.07523528 +.00000000 +00000-0 +84002-3 0 00009
2 36869 20.1592 37.6175 4451663 180.7708 178.2618 6.62658089 05
| Epoch (UTC): | 09 June 2026 01:48:20 |
| Eccentricity: | 0.4451663 |
| inclination: | 20.1592° |
| perigee height: | 265 km |
| apogee height: | 10925 km |
| right ascension of ascending node: | 37.6175° |
| argument of perigee: | 180.7708° |
| revolutions per day: | 6.62658089 |
| mean anomaly at epoch: | 178.2618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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