▸Orbital parameters

Orbit class	SSO
Inclination	97.3968°
Eccentricity	0.0007106
Period	94.7 min
Apogee	508 km
Perigee	499 km
Mean motion	15.20789486 rev/day
RAAN	85.6257°
Arg of perigee	346.3861°
Mean anomaly	13.7182°
B*	1.4763e-4
Rev at epoch	984

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 69012U 26100AJ 26188.15255375 .00003186 00000-0 14763-3 0 9997

2 69012 97.3968 85.6257 0007106 346.3861 13.7182 15.20789486 9843

▸ source OMM (JSON)

{
  "OBJECT_NAME": "JACKAL-004",
  "OBJECT_ID": "2026-100AJ",
  "EPOCH": "2026-07-07T03:39:40.644+00:00",
  "MEAN_MOTION": 15.20789486,
  "ECCENTRICITY": 0.0007106,
  "INCLINATION": 97.3968,
  "RA_OF_ASC_NODE": 85.6257,
  "ARG_OF_PERICENTER": 346.3861,
  "MEAN_ANOMALY": 13.7182,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 69012,
  "REV_AT_EPOCH": 984,
  "BSTAR": 0.00014763,
  "MEAN_MOTION_DOT": 0.00003186,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	JACKAL-004
Operator	True Anomaly Inc.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	May 3, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	275HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/69012

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.