▸Orbital parameters

Orbit class	LEO
Inclination	37.0219°
Eccentricity	0.0002506
Period	95.4 min
Apogee	540 km
Perigee	537 km
Mean motion	15.09347634 rev/day
RAAN	144.0198°
Arg of perigee	348.2506°
Mean anomaly	11.8181°
B*	2.5239e-4
Rev at epoch	27,030

▸Two-line element set (TLE)

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

1 49052U 21068A 26188.20065632 .00004025 00000-0 25239-3 0 9991

2 49052 37.0219 144.0198 0002506 348.2506 11.8181 15.09347634270306

▸ source OMM (JSON)

{
  "OBJECT_NAME": "MONOLITH",
  "OBJECT_ID": "2021-068A",
  "EPOCH": "2026-07-07T04:48:56.706+00:00",
  "MEAN_MOTION": 15.09347634,
  "ECCENTRICITY": 0.0002506,
  "INCLINATION": 37.0219,
  "RA_OF_ASC_NODE": 144.0198,
  "ARG_OF_PERICENTER": 348.2506,
  "MEAN_ANOMALY": 11.8181,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 49052,
  "REV_AT_EPOCH": 27030,
  "BSTAR": 0.00025239,
  "MEAN_MOTION_DOT": 0.00004025,
  "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	MONOLITH
Operator	USAF SMC/DoD Space Test ProgramHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jul 29, 2021HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	20HIGHvia 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/49052

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