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 26133.21765689 +.00000000 +00000-0 +12756-3 0 00004
2 00107 28.7757 158.0521 0494123 161.7270 200.1750 14.21986641 02
| Epoch (UTC): | 13 May 2026 05:13:25 |
| Eccentricity: | 0.0494123 |
| inclination: | 28.7757° |
| perigee height: | 463 km |
| apogee height: | 1174 km |
| right ascension of ascending node: | 158.0521° |
| argument of perigee: | 161.7270° |
| revolutions per day: | 14.21986641 |
| mean anomaly at epoch: | 200.1750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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