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 23545U 26106.20389215 +.00000000 +00000-0 +34214-3 0 00004
2 23545 69.9628 35.6458 0006648 237.1133 122.9386 14.95253879 00
| Epoch (UTC): | 16 April 2026 04:53:36 |
| Eccentricity: | 0.0006648 |
| inclination: | 69.9628° |
| perigee height: | 577 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 35.6458° |
| argument of perigee: | 237.1133° |
| revolutions per day: | 14.95253879 |
| mean anomaly at epoch: | 122.9386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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