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 21876U 26041.67051917 +.00000000 +00000-0 +14858-4 0 00006
2 21876 82.9260 287.8790 0033910 208.3722 209.9874 13.75969670 06
| Epoch (UTC): | 10 February 2026 16:05:32 |
| Eccentricity: | 0.0033910 |
| inclination: | 82.9260° |
| perigee height: | 953 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 287.8790° |
| argument of perigee: | 208.3722° |
| revolutions per day: | 13.75969670 |
| mean anomaly at epoch: | 209.9874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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