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 64157U 26145.13306397 +.00000000 +00000-0 +12428-2 0 00005
2 64157 97.6128 196.7014 0014447 0.4985 359.6252 15.03440545 05
| Epoch (UTC): | 25 May 2026 03:11:36 |
| Eccentricity: | 0.0014447 |
| inclination: | 97.6128° |
| perigee height: | 546 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 196.7014° |
| argument of perigee: | 0.4985° |
| revolutions per day: | 15.03440545 |
| mean anomaly at epoch: | 359.6252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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