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 59550U 26145.35992562 +.00000000 +00000-0 +39043-3 0 00008
2 59550 43.0004 270.2218 0001547 270.1128 89.9546 15.27592089 06
| Epoch (UTC): | 25 May 2026 08:38:17 |
| Eccentricity: | 0.0001547 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.2218° |
| argument of perigee: | 270.1128° |
| revolutions per day: | 15.27592089 |
| mean anomaly at epoch: | 89.9546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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