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 41867U 26139.99671815 +.00000000 +00000-0 +00000-0 0 00006
2 41867 10.9220 256.0682 4951304 161.9461 225.1603 1.89346256 08
| Epoch (UTC): | 19 May 2026 23:55:16 |
| Eccentricity: | 0.4951304 |
| inclination: | 10.9220° |
| perigee height: | 7556 km |
| apogee height: | 34886 km |
| right ascension of ascending node: | 256.0682° |
| argument of perigee: | 161.9461° |
| revolutions per day: | 1.89346256 |
| mean anomaly at epoch: | 225.1603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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