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 59407U 26145.26246821 +.00000000 +00000-0 +12570-4 0 00006
2 59407 43.0057 343.9871 0001069 280.4052 79.6679 15.27575292 07
| Epoch (UTC): | 25 May 2026 06:17:57 |
| Eccentricity: | 0.0001069 |
| inclination: | 43.0057° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 343.9871° |
| argument of perigee: | 280.4052° |
| revolutions per day: | 15.27575292 |
| mean anomaly at epoch: | 79.6679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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