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 00107U 26134.34058969 +.00000000 +00000-0 +13330-3 0 00004
2 00107 28.7762 151.5782 0494094 172.2090 188.6501 14.21989222 01
| Epoch (UTC): | 14 May 2026 08:10:26 |
| Eccentricity: | 0.0494094 |
| inclination: | 28.7762° |
| perigee height: | 463 km |
| apogee height: | 1174 km |
| right ascension of ascending node: | 151.5782° |
| argument of perigee: | 172.2090° |
| revolutions per day: | 14.21989222 |
| mean anomaly at epoch: | 188.6501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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