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 43024U 26145.58158834 +.00000000 +00000-0 +18798-3 0 00002
2 43024 97.4768 248.4756 0005859 330.4948 29.5963 15.33406094 09
| Epoch (UTC): | 25 May 2026 13:57:29 |
| Eccentricity: | 0.0005859 |
| inclination: | 97.4768° |
| perigee height: | 462 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 248.4756° |
| argument of perigee: | 330.4948° |
| revolutions per day: | 15.33406094 |
| mean anomaly at epoch: | 29.5963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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