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 10061U 26062.96622331 +.00000000 +00000-0 +00000-0 0 00009
2 10061 6.6702 294.2228 0013890 47.6111 284.7400 0.99397546 08
| Epoch (UTC): | 03 March 2026 23:11:21 |
| Eccentricity: | 0.0013890 |
| inclination: | 6.6702° |
| perigee height: | 35975 km |
| apogee height: | 36092 km |
| right ascension of ascending node: | 294.2228° |
| argument of perigee: | 47.6111° |
| revolutions per day: | 0.99397546 |
| mean anomaly at epoch: | 284.7400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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