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 37867U 26145.21532125 +.00000000 +00000-0 +00000-0 0 00003
2 37867 65.2580 73.6461 0023266 240.8621 300.4430 2.13103616 05
| Epoch (UTC): | 25 May 2026 05:10:03 |
| Eccentricity: | 0.0023266 |
| inclination: | 65.2580° |
| perigee height: | 19070 km |
| apogee height: | 19189 km |
| right ascension of ascending node: | 73.6461° |
| argument of perigee: | 240.8621° |
| revolutions per day: | 2.13103616 |
| mean anomaly at epoch: | 300.4430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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