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 43461U 26145.38639411 +.00000000 +00000-0 +71848-4 0 00006
2 43461 98.4558 116.4963 0002598 124.6440 235.5005 14.60586669 05
| Epoch (UTC): | 25 May 2026 09:16:24 |
| Eccentricity: | 0.0002598 |
| inclination: | 98.4558° |
| perigee height: | 689 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 116.4963° |
| argument of perigee: | 124.6440° |
| revolutions per day: | 14.60586669 |
| mean anomaly at epoch: | 235.5005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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