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 67188U 26145.54230750 +.00000000 +00000-0 +52855-3 0 00005
2 67188 42.9993 237.1283 0001002 266.9603 93.1133 15.27597376 01
| Epoch (UTC): | 25 May 2026 13:00:55 |
| Eccentricity: | 0.0001002 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.1283° |
| argument of perigee: | 266.9603° |
| revolutions per day: | 15.27597376 |
| mean anomaly at epoch: | 93.1133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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