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 53220U 26145.42329966 +.00000000 +00000-0 -22419-2 0 00005
2 53220 97.4454 205.3310 0002607 138.6977 221.4448 15.05807625 01
| Epoch (UTC): | 25 May 2026 10:09:33 |
| Eccentricity: | 0.0002607 |
| inclination: | 97.4454° |
| perigee height: | 547 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.3310° |
| argument of perigee: | 138.6977° |
| revolutions per day: | 15.05807625 |
| mean anomaly at epoch: | 221.4448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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