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 24958U 97058C 98141.47161467 .63367770 12784-4 48295-3 0 2726
2 24958 51.6245 164.5505 0003515 335.2238 24.8527 16.52432061 31304
| Epoch (UTC): | 21 May 1998 11:19:07 |
| Eccentricity: | 0.0003515 |
| inclination: | 51.6245° |
| perigee height: | 131 km |
| apogee height: | 135 km |
| right ascension of ascending node: | 164.5505° |
| argument of perigee: | 335.2238° |
| revolutions per day: | 16.52432061 |
| mean anomaly at epoch: | 24.8527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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