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 21153U 26047.30901505 +.00000000 +00000-0 +10464-3 0 00005
2 21153 82.9275 6.9765 0027917 306.7550 162.9037 13.76340421 01
| Epoch (UTC): | 16 February 2026 07:24:58 |
| Eccentricity: | 0.0027917 |
| inclination: | 82.9275° |
| perigee height: | 956 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 6.9765° |
| argument of perigee: | 306.7550° |
| revolutions per day: | 13.76340421 |
| mean anomaly at epoch: | 162.9037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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