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 53213U 26145.41224909 +.00000000 +00000-0 -81137-3 0 00000
2 53213 97.4466 205.3557 0000575 90.9656 269.1637 15.05701924 09
| Epoch (UTC): | 25 May 2026 09:53:38 |
| Eccentricity: | 0.0000575 |
| inclination: | 97.4466° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 205.3557° |
| argument of perigee: | 90.9656° |
| revolutions per day: | 15.05701924 |
| mean anomaly at epoch: | 269.1637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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