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 61538U 26145.62049660 +.00000000 +00000-0 +91960-5 0 00007
2 61538 53.1595 216.7687 0001542 93.2488 266.8707 15.69746039 02
| Epoch (UTC): | 25 May 2026 14:53:30 |
| Eccentricity: | 0.0001542 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 216.7687° |
| argument of perigee: | 93.2488° |
| revolutions per day: | 15.69746039 |
| mean anomaly at epoch: | 266.8707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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