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 27394U 01051C 02123.80613619 +.21143668 +12469-4 +16966-2 0 9991
2 27394 051.6100 269.3523 0009419 308.2095 051.7922 16.38999177007092
| Epoch (UTC): | 03 May 2002 19:20:50 |
| Eccentricity: | 0.0009419 |
| inclination: | 51.6100° |
| perigee height: | 162 km |
| apogee height: | 174 km |
| right ascension of ascending node: | 269.3523° |
| argument of perigee: | 308.2095° |
| revolutions per day: | 16.38999177 |
| mean anomaly at epoch: | 51.7922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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