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 26161.58443013 +.00000000 +00000-0 +43302-3 0 00001
2 23545 69.9609 256.3514 0002761 181.6316 178.4833 14.95849197 09
| Epoch (UTC): | 10 June 2026 14:01:34 |
| Eccentricity: | 0.0002761 |
| inclination: | 69.9609° |
| perigee height: | 578 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 256.3514° |
| argument of perigee: | 181.6316° |
| revolutions per day: | 14.95849197 |
| mean anomaly at epoch: | 178.4833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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