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 21015U 26041.44500933 +.00000000 +00000-0 +92455-4 0 00002
2 21015 74.0489 98.0906 0022759 298.7522 61.1345 14.37258023 00
| Epoch (UTC): | 10 February 2026 10:40:48 |
| Eccentricity: | 0.0022759 |
| inclination: | 74.0489° |
| perigee height: | 751 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 98.0906° |
| argument of perigee: | 298.7522° |
| revolutions per day: | 14.37258023 |
| mean anomaly at epoch: | 61.1345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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