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 23608U 26159.52661656 +.00000000 +00000-0 +66803-3 0 00008
2 23608 98.2744 17.3095 0007207 80.5426 279.6639 15.54176227 03
| Epoch (UTC): | 08 June 2026 12:38:19 |
| Eccentricity: | 0.0007207 |
| inclination: | 98.2744° |
| perigee height: | 400 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 17.3095° |
| argument of perigee: | 80.5426° |
| revolutions per day: | 15.54176227 |
| mean anomaly at epoch: | 279.6639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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