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 26076.16991362 +.00000000 +00000-0 +54955-3 0 00001
2 23608 98.2867 281.4890 0006989 10.5531 349.5862 15.47811585 02
| Epoch (UTC): | 17 March 2026 04:04:40 |
| Eccentricity: | 0.0006989 |
| inclination: | 98.2867° |
| perigee height: | 418 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 281.4890° |
| argument of perigee: | 10.5531° |
| revolutions per day: | 15.47811585 |
| mean anomaly at epoch: | 349.5862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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