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 26140.55818400 +.00000000 +00000-0 +43768-4 0 00007
2 01430 98.5004 260.0153 0055740 160.8428 199.4874 14.41618170 08
| Epoch (UTC): | 20 May 2026 13:23:47 |
| Eccentricity: | 0.0055740 |
| inclination: | 98.5004° |
| perigee height: | 713 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 260.0153° |
| argument of perigee: | 160.8428° |
| revolutions per day: | 14.41618170 |
| mean anomaly at epoch: | 199.4874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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