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 28470U 26138.15996765 +.00000000 +00000-0 +10454-3 0 00009
2 28470 97.2731 292.8607 0032422 328.2525 31.6754 15.19105818 01
| Epoch (UTC): | 18 May 2026 03:50:21 |
| Eccentricity: | 0.0032422 |
| inclination: | 97.2731° |
| perigee height: | 486 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 292.8607° |
| argument of perigee: | 328.2525° |
| revolutions per day: | 15.19105818 |
| mean anomaly at epoch: | 31.6754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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