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 27002U 26098.23491142 +.00000000 +00000-0 +67254-4 0 00003
2 27002 99.7922 271.7522 0018832 315.2992 218.0373 13.70633618 02
| Epoch (UTC): | 08 April 2026 05:38:16 |
| Eccentricity: | 0.0018832 |
| inclination: | 99.7922° |
| perigee height: | 983 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 271.7522° |
| argument of perigee: | 315.2992° |
| revolutions per day: | 13.70633618 |
| mean anomaly at epoch: | 218.0373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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