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 26106.20768602 +.00000000 +00000-0 +36481-3 0 00003
2 23608 98.2820 315.9403 0005870 254.2221 105.8381 15.50179232 04
| Epoch (UTC): | 16 April 2026 04:59:04 |
| Eccentricity: | 0.0005870 |
| inclination: | 98.2820° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 315.9403° |
| argument of perigee: | 254.2221° |
| revolutions per day: | 15.50179232 |
| mean anomaly at epoch: | 105.8381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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