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 29108U 26037.53717731 +.00000000 +00000-0 +27132-3 0 00003
2 29108 98.4531 48.7327 0001142 69.1191 291.0135 14.69043759 07
| Epoch (UTC): | 06 February 2026 12:53:32 |
| Eccentricity: | 0.0001142 |
| inclination: | 98.4531° |
| perigee height: | 663 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 48.7327° |
| argument of perigee: | 69.1191° |
| revolutions per day: | 14.69043759 |
| mean anomaly at epoch: | 291.0135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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