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 67049U 26145.50193245 +.00000000 +00000-0 +56588-3 0 00001
2 67049 43.0010 324.5408 0002125 269.5517 90.5091 15.27596268 02
| Epoch (UTC): | 25 May 2026 12:02:46 |
| Eccentricity: | 0.0002125 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.5408° |
| argument of perigee: | 269.5517° |
| revolutions per day: | 15.27596268 |
| mean anomaly at epoch: | 90.5091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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