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 67730U 26145.41757551 +.00000000 +00000-0 +59706-3 0 00009
2 67730 97.2854 198.9218 0000798 103.7059 256.4273 15.33448356 08
| Epoch (UTC): | 25 May 2026 10:01:18 |
| Eccentricity: | 0.0000798 |
| inclination: | 97.2854° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.9218° |
| argument of perigee: | 103.7059° |
| revolutions per day: | 15.33448356 |
| mean anomaly at epoch: | 256.4273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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