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 53083U 26145.04809192 +.00000000 +00000-0 +20317-5 0 00001
2 53083 97.4484 326.0597 0001312 88.5926 271.5452 15.05653872 02
| Epoch (UTC): | 25 May 2026 01:09:15 |
| Eccentricity: | 0.0001312 |
| inclination: | 97.4484° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 326.0597° |
| argument of perigee: | 88.5926° |
| revolutions per day: | 15.05653872 |
| mean anomaly at epoch: | 271.5452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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