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 40070U 26032.46551699 +.00000000 +00000-0 +11390-3 0 00009
2 40070 98.0554 14.9550 0131618 130.3273 230.9512 14.55454640 07
| Epoch (UTC): | 01 February 2026 11:10:20 |
| Eccentricity: | 0.0131618 |
| inclination: | 98.0554° |
| perigee height: | 615 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 14.9550° |
| argument of perigee: | 130.3273° |
| revolutions per day: | 14.55454640 |
| mean anomaly at epoch: | 230.9512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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