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 59930U 26145.32540653 +.00000000 +00000-0 +10502-3 0 00006
2 59930 43.0001 259.6942 0001319 263.9413 96.1288 15.27577130 07
| Epoch (UTC): | 25 May 2026 07:48:35 |
| Eccentricity: | 0.0001319 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 259.6942° |
| argument of perigee: | 263.9413° |
| revolutions per day: | 15.27577130 |
| mean anomaly at epoch: | 96.1288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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