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 00029U 26083.93914243 +.00000000 +00000-0 +11449-3 0 00000
2 00029 48.3783 64.9975 0022812 266.3428 93.4877 14.78655887 09
| Epoch (UTC): | 24 March 2026 22:32:21 |
| Eccentricity: | 0.0022812 |
| inclination: | 48.3783° |
| perigee height: | 618 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 64.9975° |
| argument of perigee: | 266.3428° |
| revolutions per day: | 14.78655887 |
| mean anomaly at epoch: | 93.4877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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