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 59671U 26145.15034058 +.00000000 +00000-0 +69686-4 0 00004
2 59671 43.0057 296.9651 0003491 281.4058 78.6402 15.27573178 05
| Epoch (UTC): | 25 May 2026 03:36:29 |
| Eccentricity: | 0.0003491 |
| inclination: | 43.0057° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 296.9651° |
| argument of perigee: | 281.4058° |
| revolutions per day: | 15.27573178 |
| mean anomaly at epoch: | 78.6402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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