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 26145.40560260 +.00000000 +00000-0 +14251-3 0 00001
2 28470 97.2739 299.8376 0031953 301.9331 57.8798 15.19144562 07
| Epoch (UTC): | 25 May 2026 09:44:04 |
| Eccentricity: | 0.0031953 |
| inclination: | 97.2739° |
| perigee height: | 486 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 299.8376° |
| argument of perigee: | 301.9331° |
| revolutions per day: | 15.19144562 |
| mean anomaly at epoch: | 57.8798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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