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 01430U 26153.81488875 +.00000000 +00000-0 +78802-4 0 00006
2 01430 98.5023 273.2100 0056334 121.6416 239.0286 14.41624983 06
| Epoch (UTC): | 02 June 2026 19:33:26 |
| Eccentricity: | 0.0056334 |
| inclination: | 98.5023° |
| perigee height: | 713 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 273.2100° |
| argument of perigee: | 121.6416° |
| revolutions per day: | 14.41624983 |
| mean anomaly at epoch: | 239.0286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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