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 67732U 26145.40941814 +.00000000 +00000-0 +50415-3 0 00005
2 67732 97.2856 198.9334 0000802 98.6726 261.4608 15.33446337 05
| Epoch (UTC): | 25 May 2026 09:49:33 |
| Eccentricity: | 0.0000802 |
| inclination: | 97.2856° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.9334° |
| argument of perigee: | 98.6726° |
| revolutions per day: | 15.33446337 |
| mean anomaly at epoch: | 261.4608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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