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 53080U 26145.38592235 +.00000000 +00000-0 +11617-3 0 00003
2 53080 97.4454 326.4157 0000984 111.2508 248.8824 15.05650869 09
| Epoch (UTC): | 25 May 2026 09:15:43 |
| Eccentricity: | 0.0000984 |
| inclination: | 97.4454° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 326.4157° |
| argument of perigee: | 111.2508° |
| revolutions per day: | 15.05650869 |
| mean anomaly at epoch: | 248.8824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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