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 61221U 26145.50286192 +.00000000 +00000-0 +27478-3 0 00007
2 61221 98.0423 235.6521 0001404 155.3304 204.7971 14.72296968 08
| Epoch (UTC): | 25 May 2026 12:04:07 |
| Eccentricity: | 0.0001404 |
| inclination: | 98.0423° |
| perigee height: | 653 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 235.6521° |
| argument of perigee: | 155.3304° |
| revolutions per day: | 14.72296968 |
| mean anomaly at epoch: | 204.7971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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