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 67295U 26145.14625149 +.00000000 +00000-0 +30943-3 0 00004
2 67295 97.3944 220.4268 0011801 72.6114 287.6412 15.23797774 05
| Epoch (UTC): | 25 May 2026 03:30:36 |
| Eccentricity: | 0.0011801 |
| inclination: | 97.3944° |
| perigee height: | 486 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 220.4268° |
| argument of perigee: | 72.6114° |
| revolutions per day: | 15.23797774 |
| mean anomaly at epoch: | 287.6412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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