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 53054U 26145.46348014 +.00000000 +00000-0 -15499-3 0 00000
2 53054 97.4506 326.5498 0000499 144.5169 215.6091 15.05631511 01
| Epoch (UTC): | 25 May 2026 11:07:24 |
| Eccentricity: | 0.0000499 |
| inclination: | 97.4506° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 326.5498° |
| argument of perigee: | 144.5169° |
| revolutions per day: | 15.05631511 |
| mean anomaly at epoch: | 215.6091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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