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 02980U 26088.16158509 +.00000000 +00000-0 +10100-3 0 00006
2 02980 99.1868 155.0395 0093079 355.9014 4.1412 14.62910769 02
| Epoch (UTC): | 29 March 2026 03:52:40 |
| Eccentricity: | 0.0093079 |
| inclination: | 99.1868° |
| perigee height: | 618 km |
| apogee height: | 750 km |
| right ascension of ascending node: | 155.0395° |
| argument of perigee: | 355.9014° |
| revolutions per day: | 14.62910769 |
| mean anomaly at epoch: | 4.1412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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