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 67963U 26145.47521127 +.00000000 +00000-0 +39669-3 0 00007
2 67963 97.2843 155.4489 0000986 96.2532 263.8823 15.33454063 08
| Epoch (UTC): | 25 May 2026 11:24:18 |
| Eccentricity: | 0.0000986 |
| inclination: | 97.2843° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4489° |
| argument of perigee: | 96.2532° |
| revolutions per day: | 15.33454063 |
| mean anomaly at epoch: | 263.8823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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