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 23612U 95035 A 95203.30277778 .00002218 -70109-5 +00000-0 0 9992
2 23612 028.4626 261.7787 0021123 241.6630 237.4205 15.90792464001396
| Epoch (UTC): | 22 July 1995 07:16:00 |
| Eccentricity: | 0.0021123 |
| inclination: | 28.4626° |
| perigee height: | 286 km |
| apogee height: | 314 km |
| right ascension of ascending node: | 261.7787° |
| argument of perigee: | 241.6630° |
| revolutions per day: | 15.90792464 |
| mean anomaly at epoch: | 237.4205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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