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 67837U 26145.47464723 +.00000000 +00000-0 +69282-3 0 00009
2 67837 43.0002 193.7257 0002307 295.6923 64.3690 15.27594394 01
| Epoch (UTC): | 25 May 2026 11:23:29 |
| Eccentricity: | 0.0002307 |
| inclination: | 43.0002° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 193.7257° |
| argument of perigee: | 295.6923° |
| revolutions per day: | 15.27594394 |
| mean anomaly at epoch: | 64.3690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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