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 25167U 98009A 98092.91648523 .00091113 37909-5 10211-3 0 9999
2 25167 070.3588 218.7944 0086303 162.2906 198.1352 16.01870962 7168
| Epoch (UTC): | 02 April 1998 21:59:44 |
| Eccentricity: | 0.0086303 |
| inclination: | 70.3588° |
| perigee height: | 212 km |
| apogee height: | 326 km |
| right ascension of ascending node: | 218.7944° |
| argument of perigee: | 162.2906° |
| revolutions per day: | 16.01870962 |
| mean anomaly at epoch: | 198.1352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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