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 41888U 26145.08063154 +.00000000 +00000-0 +31792-3 0 00002
2 41888 34.9444 34.8793 0009933 313.2928 46.6968 15.58648863 08
| Epoch (UTC): | 25 May 2026 01:56:06 |
| Eccentricity: | 0.0009933 |
| inclination: | 34.9444° |
| perigee height: | 385 km |
| apogee height: | 398 km |
| right ascension of ascending node: | 34.8793° |
| argument of perigee: | 313.2928° |
| revolutions per day: | 15.58648863 |
| mean anomaly at epoch: | 46.6968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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