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 53221U 26145.45103413 +.00000000 +00000-0 -18530-4 0 00007
2 53221 97.4491 205.4302 0002760 133.7790 226.3665 15.05658962 07
| Epoch (UTC): | 25 May 2026 10:49:29 |
| Eccentricity: | 0.0002760 |
| inclination: | 97.4491° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.4302° |
| argument of perigee: | 133.7790° |
| revolutions per day: | 15.05658962 |
| mean anomaly at epoch: | 226.3665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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