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 67089U 26145.33881749 +.00000000 +00000-0 +24938-3 0 00003
2 67089 70.0013 181.3976 0003534 268.3822 91.6933 14.98338157 04
| Epoch (UTC): | 25 May 2026 08:07:53 |
| Eccentricity: | 0.0003534 |
| inclination: | 70.0013° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 181.3976° |
| argument of perigee: | 268.3822° |
| revolutions per day: | 14.98338157 |
| mean anomaly at epoch: | 91.6933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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