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 67589U 26145.43432706 +.00000000 +00000-0 +51964-3 0 00003
2 67589 97.2846 210.5266 0000802 101.3423 258.7910 15.33448741 01
| Epoch (UTC): | 25 May 2026 10:25:25 |
| Eccentricity: | 0.0000802 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.5266° |
| argument of perigee: | 101.3423° |
| revolutions per day: | 15.33448741 |
| mean anomaly at epoch: | 258.7910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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