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 67693U 26145.54484008 +.00000000 +00000-0 +63903-3 0 00009
2 67693 97.2843 257.1923 0000912 116.6872 243.4464 15.33427810 09
| Epoch (UTC): | 25 May 2026 13:04:34 |
| Eccentricity: | 0.0000912 |
| inclination: | 97.2843° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1923° |
| argument of perigee: | 116.6872° |
| revolutions per day: | 15.33427810 |
| mean anomaly at epoch: | 243.4464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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