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 59477U 26145.35523010 +.00000000 +00000-0 -16400-3 0 00007
2 59477 42.9969 266.3992 0000761 294.1374 65.9398 15.27562361 02
| Epoch (UTC): | 25 May 2026 08:31:31 |
| Eccentricity: | 0.0000761 |
| inclination: | 42.9969° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.3992° |
| argument of perigee: | 294.1374° |
| revolutions per day: | 15.27562361 |
| mean anomaly at epoch: | 65.9398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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