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 67709U 26145.28110147 +.00000000 +00000-0 +10172-2 0 00007
2 67709 97.2837 256.9431 0001374 86.4693 273.6707 15.33456710 05
| Epoch (UTC): | 25 May 2026 06:44:47 |
| Eccentricity: | 0.0001374 |
| inclination: | 97.2837° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 256.9431° |
| argument of perigee: | 86.4693° |
| revolutions per day: | 15.33456710 |
| mean anomaly at epoch: | 273.6707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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