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 67742U 26145.38766561 +.00000000 +00000-0 +52411-3 0 00005
2 67742 97.2858 198.9630 0001202 90.7624 269.3756 15.33459053 02
| Epoch (UTC): | 25 May 2026 09:18:14 |
| Eccentricity: | 0.0001202 |
| inclination: | 97.2858° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.9630° |
| argument of perigee: | 90.7624° |
| revolutions per day: | 15.33459053 |
| mean anomaly at epoch: | 269.3756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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