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 24701U 96073A 97007.00481110 .00023179 79810-5 38031-4 0 203
2 24701 62.8023 198.8518 0115737 109.1102 252.3079 15.92753966 2143
| Epoch (UTC): | 07 January 1997 00:06:55 |
| Eccentricity: | 0.0115737 |
| inclination: | 62.8023° |
| perigee height: | 217 km |
| apogee height: | 372 km |
| right ascension of ascending node: | 198.8518° |
| argument of perigee: | 109.1102° |
| revolutions per day: | 15.92753966 |
| mean anomaly at epoch: | 252.3079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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