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 67293U 26145.14832639 +.00000000 +00000-0 +17260-3 0 00003
2 67293 97.3940 220.2717 0012550 72.8857 287.3753 15.22600928 02
| Epoch (UTC): | 25 May 2026 03:33:35 |
| Eccentricity: | 0.0012550 |
| inclination: | 97.3940° |
| perigee height: | 489 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 220.2717° |
| argument of perigee: | 72.8857° |
| revolutions per day: | 15.22600928 |
| mean anomaly at epoch: | 287.3753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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