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 43488U 26145.45994022 +.00000000 +00000-0 +00000-0 0 00003
2 43488 0.0407 69.8361 0001229 242.3653 191.4311 1.00272044 02
| Epoch (UTC): | 25 May 2026 11:02:18 |
| Eccentricity: | 0.0001229 |
| inclination: | 0.0407° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 69.8361° |
| argument of perigee: | 242.3653° |
| revolutions per day: | 1.00272044 |
| mean anomaly at epoch: | 191.4311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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