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 64129U 26145.63449883 +.00000000 +00000-0 +10166-2 0 00004
2 64129 42.9993 229.7718 0001544 255.4498 104.6199 15.70848503 08
| Epoch (UTC): | 25 May 2026 15:13:40 |
| Eccentricity: | 0.0001544 |
| inclination: | 42.9993° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 229.7718° |
| argument of perigee: | 255.4498° |
| revolutions per day: | 15.70848503 |
| mean anomaly at epoch: | 104.6199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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