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 53216U 26145.42055611 +.00000000 +00000-0 -87684-3 0 00009
2 53216 97.4452 205.3514 0000408 114.5801 245.5468 15.05711299 06
| Epoch (UTC): | 25 May 2026 10:05:36 |
| Eccentricity: | 0.0000408 |
| inclination: | 97.4452° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 205.3514° |
| argument of perigee: | 114.5801° |
| revolutions per day: | 15.05711299 |
| mean anomaly at epoch: | 245.5468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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