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 43476U 18047A 26152.04245354 +.00003742 00000-0 +99354-4 0 00
2 43476 88.9923 200.1747 0012215 159.5703 288.0368 15.38148018447321
| Epoch (UTC): | 01 June 2026 01:01:07 |
| Eccentricity: | 0.0012215 |
| inclination: | 88.9923° |
| perigee height: | 443 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 200.1747° |
| argument of perigee: | 159.5703° |
| revolutions per day: | 15.38148018 |
| mean anomaly at epoch: | 288.0368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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