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 26071.96733545 +.00000000 +00000-0 +77517-3 0 00000
2 23608 98.2878 276.6770 0007242 25.7596 334.4011 15.47478718 05
| Epoch (UTC): | 12 March 2026 23:12:57 |
| Eccentricity: | 0.0007242 |
| inclination: | 98.2878° |
| perigee height: | 419 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 276.6770° |
| argument of perigee: | 25.7596° |
| revolutions per day: | 15.47478718 |
| mean anomaly at epoch: | 334.4011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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