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 59481U 26145.47654439 +.00000000 +00000-0 +43860-4 0 00005
2 59481 98.7166 153.7305 0005417 39.7599 320.3974 14.20732342 05
| Epoch (UTC): | 25 May 2026 11:26:13 |
| Eccentricity: | 0.0005417 |
| inclination: | 98.7166° |
| perigee height: | 819 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 153.7305° |
| argument of perigee: | 39.7599° |
| revolutions per day: | 14.20732342 |
| mean anomaly at epoch: | 320.3974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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