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 41599U 26152.18720941 +.00000000 +00000-0 +28320-3 0 00007
2 41599 97.4489 212.3841 0009915 181.3114 178.8097 15.19348988 01
| Epoch (UTC): | 01 June 2026 04:29:34 |
| Eccentricity: | 0.0009915 |
| inclination: | 97.4489° |
| perigee height: | 501 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 212.3841° |
| argument of perigee: | 181.3114° |
| revolutions per day: | 15.19348988 |
| mean anomaly at epoch: | 178.8097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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