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 25533U 98062C 99011.27784502 .36532436 12708-4 37292-3 0 1316
2 25533 51.6341 60.1503 0001083 50.3915 309.7247 16.50803227 9678
| Epoch (UTC): | 11 January 1999 06:40:05 |
| Eccentricity: | 0.0001083 |
| inclination: | 51.6341° |
| perigee height: | 136 km |
| apogee height: | 138 km |
| right ascension of ascending node: | 60.1503° |
| argument of perigee: | 50.3915° |
| revolutions per day: | 16.50803227 |
| mean anomaly at epoch: | 309.7247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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