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 12888U 81100 B 89286.21132336 .21566456 +90000-5 +27320-3 0 9997
2 12888 097.5112 350.5628 0009533 229.8950 130.4404 16.49270150447600
| Epoch (UTC): | 13 October 1989 05:04:18 |
| Eccentricity: | 0.0009533 |
| inclination: | 97.5112° |
| perigee height: | 135 km |
| apogee height: | 147 km |
| right ascension of ascending node: | 350.5628° |
| argument of perigee: | 229.8950° |
| revolutions per day: | 16.49270150 |
| mean anomaly at epoch: | 130.4404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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