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 26039.70634950 +.00000000 +00000-0 +30783-4 0 00006
2 21876 82.9263 289.3399 0033832 214.0108 200.3399 13.75969676 09
| Epoch (UTC): | 08 February 2026 16:57:08 |
| Eccentricity: | 0.0033832 |
| inclination: | 82.9263° |
| perigee height: | 953 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 289.3399° |
| argument of perigee: | 214.0108° |
| revolutions per day: | 13.75969676 |
| mean anomaly at epoch: | 200.3399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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