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 59402U 26145.58554560 +.00000000 +00000-0 +55048-5 0 00006
2 59402 43.0021 342.1092 0001062 274.5680 85.5050 15.27577380 02
| Epoch (UTC): | 25 May 2026 14:03:11 |
| Eccentricity: | 0.0001062 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.1092° |
| argument of perigee: | 274.5680° |
| revolutions per day: | 15.27577380 |
| mean anomaly at epoch: | 85.5050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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