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 41872U 16062D 23097.15550821 .11138107 12259-4 10830-2 0 9994
2 41872 51.6348 345.3724 0009865 245.5325 114.4672 16.37347696355508
| Epoch (UTC): | 07 April 2023 03:43:55 |
| Eccentricity: | 0.0009865 |
| inclination: | 51.6348° |
| perigee height: | 166 km |
| apogee height: | 179 km |
| right ascension of ascending node: | 345.3724° |
| argument of perigee: | 245.5325° |
| revolutions per day: | 16.37347696 |
| mean anomaly at epoch: | 114.4672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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